DISSIPATIVITY BASED ANTI-DISTURBANCE EVENT-TRIGGERED TRACKING CONTROL OF TIME-DELAY SWITCHED LINEAR SYSTEMS AND ITS APPLICATION TO THE CONVERSION MODE OF XV-15 TILT-ROTOR AIRCRAFT

被引：1

作者：

Shao, Shuyi ^{[1
]}

Xia, Ranlong ^{[1
]}

Li, Wen ^{[1
]}

Wu, Qingxian ^{[1
]}

Feng, Ke ^{[2
]}

Chen, Hongtian ^{[3
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Peoples R China

[2] Univ British Columbia, Sch Engn, Kelowna, BC V1V 1V7, Canada

[3] Univ Alberta, Dept Chemicaland Mat Engn, Edmonton, AB T6G 1H9, Canada

来源：

DISCRETE AND CONTINUOUS DYNAMICAL SYSTEMS-SERIES S | 2023年 / 16卷 / 07期

基金：

中国博士后科学基金; 中国国家自然科学基金;

关键词：

Time-delay switched systems; state tracking control; quasi dissipativ-ity; XV-15 tilt-rotor aircraft; MARKOVIAN JUMP SYSTEMS; NEUTRAL SYSTEMS; STABILITY; FEEDBACK;

D O I：

10.3934/dcdss.2023090

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

In this paper, a dissipativity-based tracking problem is studied for the time-delay switched linear system with disturbances. First, a composite disturbance observer is designed to estimate the nonlinear modeling disturbances and suppress the external disturbances with bounded energy. Then, to eliminate the adverse effects of time-delay on the system, the LyapunovKrasovskii functional is designed, and the feasible conditions related to the time-delay are established. In addition, the switch tracking controller is designed by combining the dissipation theory and the average dwell time technology. Furthermore, to reduce the quantity of signal transmission in the control process, an event-triggered control scheme is designed, and the trigger threshold function related to the tracking error is introduced, so that the trigger interval is adjusted with the tracking error. Using the Lyapunov theory and Jensen inequality method with low conservatism, a set of linear matrix inequality conditions are acquired. Finally, the simulation analysis of the conversion mode of XV-15 tilt-rotor aircraft shows that the proposed scheme is effective.

引用

页码：1944 / 1963

页数：20

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